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EP 3 321 516 B1 |
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EUROPEAN PATENT SPECIFICATION |
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Mention of the grant of the patent: |
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13.05.2020 Bulletin 2020/20 |
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Date of filing: 09.11.2016 |
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International Patent Classification (IPC):
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SERVOVALVE
SERVOVENTIL
SERVOVALVE
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Designated Contracting States: |
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AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL
NO PL PT RO RS SE SI SK SM TR |
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Date of publication of application: |
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16.05.2018 Bulletin 2018/20 |
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Proprietor: Hamilton Sundstrand Corporation |
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Charlotte, NC 28277 (US) |
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Inventor: |
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- WIKTORKO, Lukasz
50-367 Wroclaw (PL)
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Representative: Dehns |
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St. Bride's House
10 Salisbury Square London EC4Y 8JD London EC4Y 8JD (GB) |
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References cited: :
EP-A1- 0 012 743 DE-A1- 4 311 218 US-A1- 2014 042 346
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WO-A1-01/59306 DE-A1- 4 431 600
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Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
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TECHNICAL FIELD
[0001] The present disclosure relates to servovalves used to transfer quantities of, or
manage the flow of fluid e.g. air.
BACKGROUND
[0002] Servovalves find a wide range of applications for controlling air or other fluid
flow to effect driving or control of another part e.g. an actuator.
[0003] A servovalve assembly includes a motor controlled by a control current which controls
flow to an air valve to control an actuator. Generally, a servovalve transforms an
input control signal into movement of an actuator cylinder. The actuator controls
e.g. an air valve. In other words, a servovalve acts as a controller, which commands
the actuator, which changes the position of an air valve's (e.g. a so-called butterfly
valve's) flow modulating feature.
[0004] Such mechanisms are used, for example, in various parts of aircraft where the management
of air/fluid flow is required, such as in engine bleeding systems, anti-ice systems,
air conditioning systems and cabin pressure systems. Servovalves are widely used to
control the flow and pressure of pneumatic and hydraulic fluids to an actuator, and
in applications where accurate position or flow rate control is required.
[0005] Conventionally, servovalve systems operate by obtaining pressurised fluid from a
high pressure source which is transmitted through a load from which the fluid is output
as a control fluid. Various types of servovalves are known - see e.g.
GB 2104249,
US 2015/0047729 and
US 9,309,900.
DE 4431600 also describes a servovalve assembly.
[0006] Electrohydraulic servovalves can have a first stage with a motor, e.g. an electrical
or electromagnetic force motor or torque motor, controlling flow of a hydraulic fluid
to drive a valve member e.g. a spool valve of a second stage, which, in turn, can
control flow of hydraulic fluid to an actuator for driving a load. The motor can operate
to position a moveable member, such as a flapper, in response to an input drive signal
or control current, to drive the second stage valve member e.g. a spool valve.
[0007] Particularly in aircraft applications, but also in other applications, servovalves
are often required to operate at various pressures and temperatures. For e.g. fast
acting air valve actuators, relatively large flows are required depending on the size
of the actuator and the valve slew rate. For such high flow rates, however, large
valve orifice areas are required. For 'flapper' type servovalves, problems arise when
dealing with large flows due to the fact that flow force acts in the direction of
the flapper movement and the motor is forced to overcome the flow forces. For clevis-like
metering valves such as described in
US 4,046,061 and
US 6,786,238, the flow forces, proportional to the flow, act simultaneously in opposite directions
so that the clevis is balanced and centered. The clevis, however, needs to be big
due to the requirement for bigger orifices to handle larger flows.
[0008] Jet pipe servovalves provide an alternative to 'flapper'- type servovalves. Jet pipe
servovalves are usually larger than flapper type servovalves but are less sensitive
to contamination. In jet pipe systems, fluid is provided via a jet pipe to a nozzle
which directs a stream of fluid at a receiver. When the nozzle is centered - i.e.
no current from the motor causes it to turn, the receiver is hit by the stream of
fluid from the nozzle at the centre so that the fluid is directed to both ends of
the spool equally. If the motor causes the nozzle to turn, the stream of fluid from
the nozzle impinges more on one side of the receiver and thus on one side of the spool
more than the other causing the spool to shift. The spool shifts until the spring
force of a feedback spring produces a torque equal to the motor torque. At this point,
the nozzle is centred again, pressure is equal on both sides of the receiver and the
spool is held in the centered position. A change in motor current moves the spool
to a new position corresponding to the applied current.
[0009] As mentioned above, jet pipe servovalves are advantageous in that they are less sensitive
to contamination e.g. in the supply fluid or from the valve environment. These valves
are, however, more complex and bulkier. The torque motor that comprises electromagnets
to apply electromagnetic force to an armature to move the jet pipe is large and heavy,
which adds to the size, weight and complexity of the overall system.
[0010] There is a need for a servovalve arrangement that can handle large fluid flows effectively,
whilst retaining a light, simple and compact design.
[0011] The present invention provides a servovalve as defined by claim 1.
[0012] The fluid transfer valve assembly may also comprise a return port for pressure returning
through the assembly.
[0013] The steerable member may comprise a flapper-type member or a jet-pipe with nozzle
which can be steered in response to the control signal. The steerable member may be
mounted within an armature and/or a flexible pipe.
[0014] In a jet-pipe system, a nozzle is preferably provided at an end of a jet pipe closest
to the valve assembly and fluid from the nozzle is directed into the valve assembly
via a receiver. The receiver is preferably configured such that when the nozzle is
in a central position, fluid enters the valve assembly evenly via both sides of the
receiver, e.g. by opposing lateral receiver channels. When the nozzle is steered to
an off-centre position, more fluid flows to one side of the valve assembly than the
other via the receiver; e.g. more flows through one lateral receiver channel than
the other.
[0015] The piezoelectric actuator means comprises a plurality of piezoelectric elements
arranged to impart movement to the steerable member. According to the invention, the
piezoelectric actuator means comprises two piezoelectric elements mounted on opposite
sides of the steerable member.
[0016] Preferred embodiments will now be described with reference to the drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0017]
Fig. 1 is a schematic view of a conventional jet pipe servovalve.
Fig. 2A is a simplified view of a conventional servovalve.
Fig. 2B is a simplified view of a servovalve according to the invention.
DETAILED DESCRIPTION
[0018] A servovalve as described below can, for example, be used in an actuator control
system. The servovalve is controlled by a torque motor to control a control flow of
fluid that is output via e.g. a butterfly value to control the movement of an actuator.
[0019] With reference to Fig. 2A, a conventional jet pipe servovalve will first be described.
The arrangement comprises a servovalve assembly have a torque motor 1 and a moveable
spool 4 mounted in a supporting block 5. The spool 4 is part of a spool assembly having:
supply ports 14, control ports 15, and a return port 16. Flow is possible between
the ports via a passage through the spool 4. The torque motor 1 provides current that
moves an armature 40 that causes a jet pipe 18 to turn at its end closest to the spool,
which end terminates in a nozzle 19. Supply fluid is provided from the supply port,
via a supply pipe 20, which may include a filter 50, to the top of the jet pipe -
i.e. the end opposite the end with the nozzle 19, and the supply fluid flows through
the jet pipe and out of the nozzle 19. A receiver 21 is provided in the block below
the nozzle. The receiver provides two channels 21a,21b via which fluid from the nozzle
19 flows into the spool 4. When no current is applied by the motor to the jet pipe,
the nozzle 19 is centered relative to the receiver 21 and supply fluid exiting the
nozzle flows equally through both channels 21a, 21b and thus equally to both ends
of the spool 4. The spool therefore remains centered - i.e. 'closed' so that no fluid
flows through the control ports. When actuator control is desired, the motor provides
a control current to the jet pipe via the armature 40 causing the nozzle to turn away
from the centered position. The jet pipe and nozzle are turned due to an electromagnetic
force created by electromagnets of the torque motor 1 acting on the armature which
acts on the jet pipe. The supply fluid through the nozzle 19 then flows predominantly
through one receiver channel 21a or 21b as compared to the other channel. More fluid
flows, therefore, into the corresponding end of the spool 4 causing axial movement
of the spool 4 with either blocks/occludes the passage between the supply port and
the respective control port or opens the passage to allow flow between the two ports,
depending on the axial position of the spool due to the position of the nozzle 19,
thus modulating pressure on the control ports 15 and controlling the actuator (not
shown).
[0020] In an example, the assembly is arranged to control an actuator based on the fluid
flow from the control port 15 e.g. via a butterfly valve. The servovalve controls
an actuator which, in turn, controls an air valve such as a butterfly valve.
[0021] Supply pressure is provided to the spool 4 via spool supply ports 14. The pressure
at return port 16 is atmospheric pressure which will vary depending e.g. on the altitude
of the aircraft in flight. Control ports 15 provide a controlled pressure, dependant
on the nozzle position and resulting spool position, to be provided to an actuator.
A supply pipe 20 is also connected to the supply port and routes supply fluid external
to the spool and into the top end of the jet pipe 18. The supply fluid flows down
the jet pipe 18 to the nozzle 19 and exits to the receiver 21 described above. The
jet pipe 18 is preferably mounted in a flexural tube 26. While the nozzle 19 is centered
as shown in Fig. 1, equal amounts of fluid go to the two ends 4a,4b of the spool 4.
[0022] The spool 4 is in the form of a tubular member arranged in the block 5 to be moved
axially by fluid from the jet pipe 18 via the nozzle 19 that is directed at the spool
4 via the receiver 21.
[0023] The feedback spring 27 serves to return the nozzle to the centered position.
[0024] In more detail, in the embodiment shown, to open the servovalve, control current
is provided to coils of the motor (here a torque motor) creating electromagnetic torque
opposing the sum of mechanical and magnetic torque already 'present' in the torque
motor 1. The bigger the electromagnetic force from the coils, the more the jet pipe
nozzle turns. The more it turns, the greater the linear or axial movement of the spool
4. A torque motor usually consists of coil windings, a ferromagnetic armature, permanent
magnets and a mechanical spring (here two torsional bridge shafts).
[0025] This arrangement provides movement of the nozzle 19 proportional to the input control
current. Other types of motor could be envisaged.
[0026] According to the present invention, the torque motor is replaced by a piezoelectric
actuator configured to cause movement of the jet pipe, in a jet pipe system, or of
the flapper in a flapper-type system. This is shown, in an example, in Fig. 2B which
can be compared with the conventional system of Fig. 2A.
[0027] Instead of the torque motor 1, a piezoelectric actuator is positioned around the
jet pipe. Preferably, the piezoelectric actuator comprises two opposing piezoelectric
elements 60a, 60b acting on the jet pipe from opposite sides. Operation of the elements
will, via an elastic element 70a, 70b, cause the jet pipe and hence the nozzle to
move responsive to the control signal to vary the flow to the ends 4a, 4b of the spool
via the receiver channels 21a, 21b. The piezoelectric actuator can be located anywhere
along the jet pipe and the location can be selected based, e.g. on the size of the
piezoelectric elements.
[0028] It is also conceivable to replace the torque motor with a piezoelectric actuator
in a flapper-type servovalve although this is not shown in the drawings. The position
of the flapper element would be controlled by the piezoelectric force as with the
jet pipe.
[0029] Operation of the spool and feedback is as in conventional systems.
[0030] The system of this disclosure has fewer component parts than conventional systems
and the assembly is simpler, lighter and less expensive.
[0031] Although this disclosure has been described in terms of preferred examples, it should
be understood that these examples are illustrative only and modifications and alterations
are possible within the scope of the claims.
1. A servovalve comprising: a fluid transfer valve assembly comprising a supply port
(14) and a control port (15); a moveable valve spool (4) arranged to regulate flow
of fluid from the supply port to the control port in response to a control signal;
and a drive assembly (18', 19') configured to axially move the valve spool relative
to the fluid transfer assembly in response to the control signal to regulate the fluid
flow; wherein the drive assembly comprises a steerable member moveable by an amount
determined by the control signal to cause corresponding movement of the valve spool;
the drive assembly further comprising piezoelectric actuator means (60a, 60b) configured
to move said steerable member in response to the control signal; characterised in that the piezoelectric actuator means comprises two piezoelectric elements (60a, 60b)
mounted on opposite sides of the steerable member arranged to impart movement to the
steerable member via two elastic elements (70a, 70b), one provided between each of
the piezoelectric elements and a respective side of the steerable member.
2. The servovalve of claim 1, wherein the fluid transfer valve assembly further comprises
a return port (16) for pressure returning through the assembly.
3. The servovalve of claim 1 or 2, wherein the steerable member comprises a flapper member
arranged to engage and move the spool (4) in response to the control signal.
4. The servovalve of Claim 1 or 2, wherein the steerable member comprises a jet pipe
via which fluid is directed into the valve assembly to move the spool (4) in response
to the control signal.
5. The servovalve of claim 4, wherein a nozzle is provided at an end of the jet pipe
(18') closest to the valve assembly and fluid from the nozzle is directed into the
valve assembly via a receiver (21).
6. The servovalve of Claim 5, wherein the receiver is configured such that when the nozzle
is in a central position, fluid enters the valve assembly evenly via both sides of
the receiver, when the nozzle is steered to an off-centre position, more fluid flows
to one side of the valve assembly than the other via the receiver.
7. The servovalve of Claim 5, wherein the receiver comprises lateral receiver channels
to provide flow to each side of the valve assembly.
8. The servovalve of claim 5 or any claim dependent thereon, wherein the nozzle is provided
on the jet pipe mounted within a flexible tube .
9. The servovalve of any preceding claim, wherein the piezoelectric actuator means is
mounted in a housing mounted to the valve assembly.
1. Servoventil, umfassend: eine Fluidtransferventilbaugruppe, die eine Zufuhröffnung
(14) und eine Steueröffnung (15) umfasst; eine bewegbare Ventilspule (4), die angeordnet
ist, um Fluss an Fluid von der Zufuhröffnung zu der Steueröffnung als Reaktion auf
ein Steuersignal zu regulieren; und eine Antriebsbaugruppe (18', 19'), die konfiguriert
ist, um die Ventilspule relativ zu der Fluidtransferbaugruppe als Reaktion auf das
Steuersignal axial zu bewegen, um den Fluidfluss zu regulieren; wobei die Antriebsbaugruppe
ein lenkbares Element umfasst, das um eine Menge bewegbar ist, die durch das Steuersignal
bestimmt wird, um entsprechende Bewegung der Ventilspule zu bewirken; wobei die Antriebsbaugruppe
ferner piezoelektrische Aktormittel (60a, 60b) umfasst, die konfiguriert sind, um
das lenkbare Element als Reaktion auf das Steuersignal zu bewegen;
dadurch gekennzeichnet, dass
die piezoelektrischen Aktormittel zwei piezoelektrische Elemente (60a, 60b) umfassen,
die auf gegenüberliegenden Seiten des lenkbaren Elements montiert sind, die angeordnet
sind, um dem lenkbaren Element über zwei elastische Elemente (70a, 70b), einem bereitgestellt
zwischen jedem der piezoelektrischen Elemente und einer jeweiligen Seite des lenkbaren
Elements, Bewegung zu verleihen.
2. Servoventil nach Anspruch 1, wobei die Fluidtransferventilbaugruppe ferner eine Rücklauföffnung
(16) für Druck, der durch die Baugruppe zurückkehrt, umfasst.
3. Servoventil nach Anspruch 1 oder 2, wobei das lenkbare Element ein Klappenelement
umfasst, das angeordnet ist, um die Spule (4) als Reaktion auf das Steuersignal in
Eingriff zu nehmen und zu bewegen.
4. Servoventil nach Anspruch 1 oder 2, wobei das lenkbare Element ein Strahlrohr umfasst,
über das Fluid in die Ventilbaugruppe gerichtet wird, um die Spule (4) als Reaktion
auf das Steuersignal zu bewegen.
5. Servoventil nach Anspruch 4, wobei eine Düse an einem Ende des Strahlrohrs (18') bereitgestellt
ist, das der Ventilbaugruppe am nächsten ist und Fluid aus der Düse über eine Aufnahme
(21) in die Ventilbaugruppe gerichtet wird.
6. Servoventil nach Anspruch 5, wobei die Aufnahme konfiguriert ist, sodass, wenn sich
die Düse in einer mittigen Position befindet, Fluid gleichmäßig über beide Seiten
der Aufnahme in die Ventilbaugruppe eintritt, wobei, wenn die Düse zu einer außermittigen
Position gelenkt wird, mehr Fluid über die Aufnahme zu einer Seite der Ventilbaugruppe
als der anderen fließt.
7. Servoventil nach Anspruch 5, wobei die Aufnahme seitliche Aufnahmekanäle umfasst,
um jeder Seite der Ventilbaugruppe Fluss bereitzustellen.
8. Servoventil nach Anspruch 5 oder einem davon abhängigen Anspruch, wobei die Düse an
dem Strahlrohr bereitgestellt ist, das innerhalb eines flexiblen Schlauchs montiert
ist.
9. Servoventil nach einem vorhergehenden Anspruch, wobei die piezoelektrischen Aktormittel
in einem Gehäuse montiert sind, das an der Ventilbaugruppe montiert ist.
1. Servodistributeur comprenant : un ensemble soupape de transfert de fluide comprenant
un orifice d'alimentation (14) et un orifice de commande (15) ; un tiroir de soupape
mobile (4) agencé pour réguler l'écoulement de fluide depuis l'orifice d'alimentation
vers l'orifice de commande en réponse à un signal de commande ; et un ensemble d'entraînement
(18', 19') configuré pour déplacer axialement le tiroir de soupape par rapport à l'ensemble
de transfert de fluide en réponse au signal de commande pour réguler l'écoulement
de fluide ; dans lequel l'ensemble d'entraînement comprend un élément orientable mobile
d'une quantité déterminée par le signal de commande pour entraîner un mouvement correspondant
du tiroir de soupape ; l'ensemble d'entraînement comprenant en outre des moyens d'actionnement
piézoélectriques (60a, 60b) configurés pour déplacer ledit élément orientable en réponse
au signal de commande ; caractérisé en ce que le moyen d'actionnement piézoélectrique comprend deux éléments piézoélectriques (60a,
60b) montés sur des côtés opposés de l'élément orientable agencés pour conférer un
mouvement à l'élément orientable par l'intermédiaire de deux éléments élastiques (70a,
70b), l'un prévu entre chacun des éléments piézoélectriques et un côté respectif de
l'élément orientable.
2. Servodistributeur selon la revendication 1, dans lequel l'ensemble soupape de transfert
de fluide comprend en outre un orifice de retour (16) pour le retour de pression à
travers l'ensemble.
3. Servodistributeur selon la revendication 1 ou 2, dans lequel l'élément orientable
comprend un élément clapet agencé pour venir en prise avec le tiroir (4) et déplacer
celui-ci en réponse au signal de commande.
4. Servodistributeur selon la revendication 1 ou 2, dans lequel l'élément orientable
comprend un tuyau à jet par l'intermédiaire duquel le fluide est dirigé dans l'ensemble
soupape pour déplacer le tiroir (4) en réponse au signal de commande.
5. Servodistributeur selon la revendication 4, dans lequel une buse est prévue à une
extrémité du tuyau à jet (18') la plus proche de l'ensemble soupape et le fluide de
la buse est dirigé dans l'ensemble soupape par l'intermédiaire d'un récepteur (21).
6. Servodistributeur selon la revendication 5, dans lequel le récepteur est configuré
de sorte que, lorsque la buse est dans une position centrale, du fluide pénètre dans
l'ensemble soupape uniformément par l'intermédiaire des deux côtés du récepteur, lorsque
la buse est dirigée vers une position décentrée, plus de fluide s'écoule d'un côté
de l'ensemble soupape que de l'autre par l'intermédiaire du récepteur.
7. Servodistributeur selon la revendication 5, dans lequel le récepteur comprend des
canaux de réception latéraux pour fournir un écoulement à chaque côté de l'ensemble
soupape.
8. Servodistributeur selon la revendication 5 ou une quelconque revendication dépendante
de celle-ci, dans lequel la buse est prévue sur le tuyau à jet monté à l'intérieur
d'un tube flexible.
9. Servodistributeur selon une quelconque revendication précédente, dans lequel le moyen
d'actionnement piézoélectrique est monté dans un boîtier monté sur l'ensemble soupape.
REFERENCES CITED IN THE DESCRIPTION
This list of references cited by the applicant is for the reader's convenience only.
It does not form part of the European patent document. Even though great care has
been taken in compiling the references, errors or omissions cannot be excluded and
the EPO disclaims all liability in this regard.
Patent documents cited in the description